T-1A MQF 2017 - Third 50 Questions

Question 1

In the event of electrical system failure, excluding the aircraft battery, placing the BATTERY switch to the EMER position causes the battery to power the _____

Answer 1

emergency bus
standby bus
standby battery
ALL OF THE ABOVE!

Question 2

During the SMOKE OR FUMES IN AIRCRAFT checklist, the bleed air source selector must remain in each position long enough (approximately ____ seconds) to allow adequate system purging to determine the source of smoke.

Answer 2

20 seconds

Question 3

With oil pressure below _____ psi, execute engine shutdown during flight checklist

Answer 3

40 psi

Question 4

If high oil temperature is experienced, _____

Answer 4

throttle on the affected engine should be increased within N1 limits

Question 5

While trying to eliminate smoke or fumes from inside the aircraft, turning the manual pressure controller fully counterclockwise will decrease the cabin pressure to the absolute pressure regulator setting of ____

Answer 5

12,500 +/- 1,500

Question 6

Under high temp, low altitude, high throttle setting conditions, engine oil temp may exceed ___ when throttles are reduced due to a reduction in cooling fuel through the fuel/oil heat exchanger. The max transient limit is ___ and ___ should not be exceeded for more than ___ minutes.

Answer 6

121 degrees C,
135 degrees C,
121 degrees C,
15 minutes

Question 7

If you have an EFC failure

Answer 7

matching the throttles using the engine with the EFC off may cause overboosting of the other engine

Question 8

If the fuel filter bypass annunciator is illuminated, the bypass filter is purifying the fuel to the engine.

Answer 8

FALSE

Question 9

Left or right fuel level low annunciator illumination indicates that approximately ___ pounds of usable fuel remain in the affected wing tank.

Answer 9

200 pounds of usable fuel

Question 10

If acceptable takeoff performance can only be achieved by selecting 0 degrees flaps and/or ACM off, takeoff in the presence of potential windshear is not recommended. Windshear conditions will quickly negate these minor performance enhancements.

Answer 10

TRUE

Question 11

If automatic starter dropout has not occurred by ___% N2, press the starter disengage button.

Answer 11

45% N2

Question 12

Autopilot engagement is not possible with the pitch trim selector in the EMER position.

Answer 12

TRUE

Question 13

An operating procedure or technique which could result in personal injury or loss of life if not carefully followed is a ___.

Answer 13

WARNING

Question 14

Ground fault protection is provided by the ___.

Answer 14

Battery protection circuits

Question 15

Air entering the cabin for pressurization during air conditioning emergency operation will still be hot until the bleed air selector has been turned off.

Answer 15

TRUE

Question 16

In the event of a bleed air duct failure annunciator illumination, if the wing anti-ice switch was in use, subsequently turned OFF and the annunciator extinguishes, flight may be continued if icing conditions are avoided.

Answer 16

TRUE

Question 17

If the AIR COND FAIL annunciator illuminates, the system will switch from normal to emergency pressure mode automatically.

Answer 17

TRUE

Question 18

Upon landing, if a malfunction occurs with an associated loss of brakes, _____.

Answer 18

Immediately place the anti-skid switch to the OFF position and attempt braking from both the pilot’s and copilot’s position. If braking is not restored, use the emergency brake system.

Question 19

The emergency descent procedure is a maximum rate descent to quickly escape the high altitude environment.

Answer 19

TRUE

Question 20

To execute an emergency descent:

Answer 20

You may use a moderate bank up to 45 degrees to aid in lowering the nose
Lower the nose approximately 20 degrees
Accelerate to 330 KIAS or .78 MACH, whichever is slower
ALL OF THE ABOVE!

Question 21

The maximum zero fuel weight is _____ pounds.

Answer 21

13,000 pounds

Question 22

During a controllability check, the aircraft speed must be decreased to a point where full control deflection is required to maintain controlled flight in order to properly evaluate handling characteristics at slow speeds.

Answer 22

FALSE

Question 23

Do not attempt an actual single engine go-around after selecting flaps to 30 degrees.

Answer 23

TRUE

Question 24

When executing a forced landing without power, if sufficient altitude remains after reaching a suitable landing area, a rectangular pattern will provide the best observation of surface condition, wind speed, and direction.

Answer 24

FALSE

Question 25

Pushing the AV STBY BLO button isolates power to the failed blower system.

Answer 25

FALSE

Question 26

Pushing the AV STBY BLO button does not isolate power to the failed blower system. If an overheat condition occurs, isolate the circuit by pulling the GALLEY circuit breaker.

Answer 26

TRUE

Question 27

Electrical loads up to ___ amps are permissible to single generator operations above 32,500 feet.

Answer 27

280 amps

Question 28

If operating below 32,500, single generator operations load capacity ____ amps.

Answer 28

400 amps

Question 29

Partial failure of the electrical system may necessitate degrading electrical systems to reduce electrical loads imposed on the operating generator.

Answer 29

TRUE

Question 30

When both generator master switches and the battery switch are placed in EMER, all electrical power except the items on the emergency bus and DC Standby Bus are lost. Which of the following will NOT occur?

Answer 30

(Answer is B.)
A. All right engine instrument indications will be lost
B. Both normal and emergency pitch trim will be lost
C. Engine EFCs will be inop, with associated thrust loss
D. Both fuel transfer pumps will be inop and the engine anti-ice valves will open

Question 31

During a dual generator failure situation, if the generators fail to reset and flight conditions permit, attempt to reset by turning both generator switches to OFF and reset them one at a time.

Answer 31

TRUE

Question 32

Illumination of the AC BUS SHED annunciator is advisory only and indicates a combination inverter/load bus malfunction that will result in the loss of flap position indicator and both oil pressure indicators.

Answer 32

TRUE

Question 33

The BATTERY FDR FAIL light on the overhead panel illuminates with any of three possible malfunctions. Which statement is correct in its entirety?

Answer 33

If the light is accompanied by only the EMER BUS FDR FAIL annunciator, check the EMER BUS FDR circuit breaker. If the circuit breaker has tripped and will not reset, subsequent loss of the left load bus will result in loss of the emergency bus.

Question 34

When the BATT CUT OFF annunciator is illuminated, it means the battery _____ and _____

Answer 34

relay is open; battery charging will not occur

Question 35

If the DOOR UNLOCK annunciator illuminates in flight, the jump seat may check the security of the cabin door as long as they stay securely fastened.

Answer 35

FALSE

Question 36

The DOOR UNLOCK annunciator indicates that:

Answer 36

(Answer is A and B)
A. The cabin door upper lock pins are not fully seated
B. the aft fuselage door is not fully closed and locked

Question 37

The CABIN PRESSURE LO warning annunciator will illuminate when the

Answer 37

cabin altitude exceeds 9,500 +/- 500 feet

Question 38

Severe windshear is that which produces airspeed changes greater than ___ knots or vertical speed changes greater than ___ fpm.

Answer 38

15 knots, 500 fpm

Question 39

Under windshear approach procedures, reference ground speed is computed by ___ the surface headwind component (or ___ the tailwind component) from the approach true airspeed.

Answer 39

SUBTRACTING (the surface headwind) or

ADDING (the tailwind component)

Question 40

An external power unit is required for engine start at ambient temperatures below ___

Answer 40

5 FAHRENHEIT

Question 41

If only two pilots are onboard, crew members will exchange seats only when the autopilot is engaged.

Answer 41

FALSE

Question 42

The Pilot Flying must announce to the crew when the autopilot is engaged or disengaged.

Answer 42

TRUE

Question 43

Only the pilot and copilot need to monitor UHF and VHF frequencies during descent when three crew members are aboard the aircraft.

Answer 43

FALSE

Question 44

The flight crew will make all necessary entries in AFTO 781 to indicate when any limitations have been exceeded. Entries shall include:

Answer 44

A. time interval (where applicable
B. actual instrument reading of the limitation that was exceeded
C. amount and duration of an over temperature
D. ALL OF THE ABOVE!

Question 45

Do not operate surface anti-ice systems in flight at ram air temperatures above 10 degrees C.

Answer 45

TRUE

Question 46

The yaw damper must be disengaged by 200 feet AGL for all landings.

Answer 46

FALSE

Question 47

With respect to brake energy limitations, the same amount of heat is generated by the brakes in stopping the aircraft within a given stopping distance, regardless of whether the brakes are applied in one steady application or in a series of short applications.

Answer 47

TRUE

Question 48

Maximum Braking Speed is the brake application speed from which the aircraft may be brought to a full stop without exceeding the energy absorption capability of the brakes. This energy absorption corresponds to the fuse plug brake energy, ___ million FT-LB per brake.

Answer 48

4.05

Question 49

When ___ million foot pounds are absorbed, thermal fused screws may release resulting in flat tires.

Answer 49

8.1

Question 50

If hot brakes are suspected.

Answer 50

A. the aircraft should not be taxied any more than necessary to clear the active rwy
B. the aircraft should not be maneuvered into a crowded parking area
C. the parking brake should not be set and do no approach overheated brakes for one half hour
D. ALL OF THE ABOVE!